DE1426792B2 - Overflow valve of a steam or gas turbine - Google Patents
Overflow valve of a steam or gas turbineInfo
- Publication number
- DE1426792B2 DE1426792B2 DE19651426792 DE1426792A DE1426792B2 DE 1426792 B2 DE1426792 B2 DE 1426792B2 DE 19651426792 DE19651426792 DE 19651426792 DE 1426792 A DE1426792 A DE 1426792A DE 1426792 B2 DE1426792 B2 DE 1426792B2
- Authority
- DE
- Germany
- Prior art keywords
- ring
- turbine
- pressure part
- overflow valve
- valve
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/105—Final actuators by passing part of the fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/023—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines the working-fluid being divided into several separate flows ; several separate fluid flows being united in a single flow; the machine or engine having provision for two or more different possible fluid flow paths
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D13/00—Combinations of two or more machines or engines
- F01D13/02—Working-fluid interconnection of machines or engines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Lift Valve (AREA)
- Control Of Turbines (AREA)
Description
der Zwischenwand 17 getragen. Zwischen dem Zwischenboden 25 und der Turbinenwelle 13 befindet sich eine Wellenlabyrinthdichtung, die aber nicht besonders dargestellt ist.the partition 17 carried. Located between the intermediate floor 25 and the turbine shaft 13 a shaft labyrinth seal, which is not particularly shown.
Das Schwenken des Ringes 14 geschieht über einen Schwenkhebel 20, der über einen Schlitz 21 an einem Bolzen 22 angreift, der in einer Bolzenhalterung 27 des Ringes 14 vorgesehen ist.The pivoting of the ring 14 takes place via a pivot lever 20, which is connected via a slot 21 a bolt 22 engages, which is provided in a bolt holder 27 of the ring 14.
Während der Ring 14 gemäß F i g. 1 beim öffnen und Schließen des Ventils über die ringförmige Ventilsitzanordnung streicht, wobei praktisch keine Treibmitteldruckkräfte auf den Ring 14 wirken, sondern nur Reibungskräfte im Gebiet der Lagerung ■■? (Bolzen 16), bewegt sich der Ring 28 gemäß Fig.2, der horizontal geteilt ist, beim öffnen vom ringförmigen, koaxialen Sitz 29 in Richtung der Pfeile 20 weg. Umgekehrt gilt das Entsprechende. Auch hier wirken keine Treibmitteldruckkräfte auf den Ring 28, son dern nur Reibungskräfte an der Lagerung (s. die Bolzen 31). Die Zwischenwand besteht hier aus zwei ringförmigen, koaxialen Teilen 32 und 33, die mittels Rippen 34 und 26 miteinander verbunden sind. Die Teile 32 und 33 sind radial geteilt Desgleichen ist der Ring 28 radial geteilt.While the ring 14 according to FIG. 1 brushes over the annular valve seat arrangement when the valve is opened and closed, with practically no propellant pressure forces acting on the ring 14, but only frictional forces in the area of the bearing ■■? (Bolt 16), the ring 28 according to FIG. 2, which is divided horizontally, moves away from the annular, coaxial seat 29 in the direction of the arrows 20 when it is opened. The reverse is also true. Here, too, no propellant pressure forces act on the ring 28, but only frictional forces on the bearing (see the bolts 31). The partition here consists of two ring-shaped, coaxial parts 32 and 33 which are connected to one another by means of ribs 34 and 26. The parts 32 and 33 are divided radially. The ring 28 is likewise divided radially.
Durch diese Bauformen sind auch Schwingungen des Ringes, wenn er sich in geöffneter oder teilweise geöffneter Stellung befindet, weitgehend unterbunden. These designs also cause the ring to vibrate when it is open or partially is in the open position, largely prevented.
Claims (1)
der Turbine entnehmbar ist, und das innerhalb eines Gemäß Fig. 1 und2 ist ein nicht dargestellterLow-pressure part of a steam or gas turbine is switched in a turbine, between which parts propellant is shown in longitudinal section. ·
the turbine is removable, and that within a According to FIGS. 1 and 2 is a not shown
eingangs angegebenen Art erfindungsgemäß dadurch In der Zwischenwand 17 befindet sich ein ko-This task is performed with an overflow valve of 65 or some other radial parting line.
initially specified type according to the invention characterized in the intermediate wall 17 is a co-
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEA0050957 | 1965-12-02 |
Publications (3)
Publication Number | Publication Date |
---|---|
DE1426792A1 DE1426792A1 (en) | 1969-03-20 |
DE1426792B2 true DE1426792B2 (en) | 1974-03-07 |
DE1426792C3 DE1426792C3 (en) | 1974-10-03 |
Family
ID=6937683
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19651426792 Expired DE1426792C3 (en) | 1965-12-02 | 1965-12-02 | Overflow valve of a steam or gas turbine |
Country Status (5)
Country | Link |
---|---|
BE (1) | BE690570A (en) |
CH (1) | CH451208A (en) |
DE (1) | DE1426792C3 (en) |
FR (1) | FR1502513A (en) |
GB (1) | GB1096990A (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2103289A (en) * | 1981-08-07 | 1983-02-16 | Gen Electric | Fluid modulation apparatus |
DE19522359C1 (en) * | 1995-06-20 | 1996-08-14 | Siemens Ag | Flow regulation component for steam turbine |
US5921747A (en) * | 1995-06-20 | 1999-07-13 | Siemens Aktiengesellschaft | Steam turbine component with throttle element for regulating steam flow and steam turbine having the steam turbine component |
-
1965
- 1965-12-02 DE DE19651426792 patent/DE1426792C3/en not_active Expired
-
1966
- 1966-11-25 CH CH1691966A patent/CH451208A/en unknown
- 1966-11-30 FR FR85644A patent/FR1502513A/en not_active Expired
- 1966-12-01 BE BE690570D patent/BE690570A/xx unknown
- 1966-12-02 GB GB5411766A patent/GB1096990A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
CH451208A (en) | 1968-05-15 |
DE1426792C3 (en) | 1974-10-03 |
GB1096990A (en) | 1967-12-29 |
BE690570A (en) | 1967-05-16 |
DE1426792A1 (en) | 1969-03-20 |
FR1502513A (en) | 1967-11-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C3 | Grant after two publication steps (3rd publication) | ||
E771 | Valid patent as to the heymanns-index 1977, willingness to grant licences | ||
EHJ | Ceased/non-payment of the annual fee |